33-1B - Turbine Engine Foreign Object Ingestion and Rotor Blade Containment Type Certification Procedures
- Date Issued
- April 22, 1970
- Responsible Office
- Provides guidance and acceptable means, not the sole means, by which compliance may be shown with the design and construction requirements of Part 33 of the Federal Aviation Regulations.
- ac33-1b.pdf (PDF, 1.26 MB)